Book:
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eBook:
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COMPOSITES TOOLBOX
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Mic-Mac|
Analysis
Type |
Smooth
Coupon |
Panel
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Failure
Envelope |
Circular
Opening |
Failure
Envelope |
Tapered
Shaft |
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Static Strength
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Optimized Laminates
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Hot-Wet Condition
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Buckling
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Vibration
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Creep Rupture
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Fatigue Life and Cycles
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Progressive Damage
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In addition to these tools, participants will get copies of Simulia Abaqus CAE v 6.9 (Student Edition).
Participants get intensive training via live demonstration and practice sessions where the participants are urged to try the software along with the online instructor.
EXAMPLES:
With the help of these easy-to-use tools, users will be
able to conduct wide range of analyses including cases as shown
in the following examples:
Example 1:
Displacement profile
in a wind turbine blade.
Example 2:
3D contour plot
tool for 3D beam: failure index and deflection profiles.
Example 3:
3D beam analysis
of aircraft fuselage with stringers and spars.
Example
4 :
Progressive damage of an open hole specimen under lateral
tension.
Example
5 :
Progressive damage failure analysis of a laminate with an
oval cutout under uniaxial X-Tension.
Example 6 :
Strength ratio
distribution of [0/45/-45]s laminate under tension: smooth and
open hole specimen
Example
7 :
Strengths (R/FPF)
of a) a UD sepcimen under homogenous stress state, b) a UD sepcimen
with stress concentrations due to test grips and c) an off axis
specimen with test grips.
Example
8 :
Buckling analysis
of a [0/+-45]2s laminate plate with an oblong hole.
Example
9 :
Optimization of ply
angles for a laminate with oblong opening under tension at one
direction and fixed BC in other direction.
Example
10 :
Frequency
analysis: first few modes of a tubular shaft under fixed-free
BC.
Example
11 :
Generation of short
term and creep rupture failure envelopes for UD lamiante
(T700/Epoxy).
Example
12 :
Generation of fatigue failure envelopes.
Example
13 :
Generation of faigue master curve.
Example
14 :
Generation of ultimate failure envelopes for the cases where
the stress state is non-homogenous.
Example
15 :
Progressive damage of Pin-Loaded holes under net shear-out
failure mode.
Example
16 :
Temperature and moisture profile through the laminate thickness
under the condition of intercontinental flight.